AU2003278524A1 - Sector-divided turbine assembly with axial piston variable-geometry mechanism - Google Patents

Sector-divided turbine assembly with axial piston variable-geometry mechanism

Info

Publication number
AU2003278524A1
AU2003278524A1 AU2003278524A AU2003278524A AU2003278524A1 AU 2003278524 A1 AU2003278524 A1 AU 2003278524A1 AU 2003278524 A AU2003278524 A AU 2003278524A AU 2003278524 A AU2003278524 A AU 2003278524A AU 2003278524 A1 AU2003278524 A1 AU 2003278524A1
Authority
AU
Australia
Prior art keywords
sector
axial piston
turbine assembly
geometry mechanism
piston variable
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
AU2003278524A
Inventor
Luciano Bernardini
Alain Lombard
Jeff Lotterman
Dominique Petitjean
Quentin Roberts
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Honeywell International Inc
Original Assignee
Honeywell International Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Honeywell International Inc filed Critical Honeywell International Inc
Publication of AU2003278524A1 publication Critical patent/AU2003278524A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/026—Scrolls for radial machines or engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
    • F01D17/143—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path the shiftable member being a wall, or part thereof of a radial diffuser
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/167—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes of vanes moving in translation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/40—Application in turbochargers
AU2003278524A 2003-10-24 2003-10-24 Sector-divided turbine assembly with axial piston variable-geometry mechanism Abandoned AU2003278524A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/IB2003/005142 WO2005040560A1 (en) 2003-10-24 2003-10-24 Sector-divided turbine assembly with axial piston variable-geometry mechanism

Publications (1)

Publication Number Publication Date
AU2003278524A1 true AU2003278524A1 (en) 2005-05-11

Family

ID=34509324

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2003278524A Abandoned AU2003278524A1 (en) 2003-10-24 2003-10-24 Sector-divided turbine assembly with axial piston variable-geometry mechanism

Country Status (4)

Country Link
US (1) US20080038110A1 (en)
EP (1) EP1725742A1 (en)
AU (1) AU2003278524A1 (en)
WO (1) WO2005040560A1 (en)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0227473D0 (en) * 2002-11-25 2002-12-31 Leavesley Malcolm G Variable turbocharger apparatus with bypass apertures
AT501234B1 (en) * 2006-03-30 2008-02-15 Avl List Gmbh GAS TURBINE FOR AN INTERNAL COMBUSTION ENGINE
US8191367B2 (en) 2005-11-16 2012-06-05 Honeywell International Inc. Sliding piston cartridge and turbocharger incorporating same
WO2007148145A1 (en) 2006-06-19 2007-12-27 Turbo Energy Limited Variable stator blade mechanism for turbochargers
FR2911386B1 (en) * 2007-01-16 2009-03-06 Genius Soc Responsabilite Limi AIR CONDITIONING APPARATUS WITH COMPRESSOR AND VORTEX
US8123470B2 (en) * 2007-08-10 2012-02-28 Honeywell International Inc. Turbine assembly with semi-divided nozzle and half-collar piston
AT505407B1 (en) * 2007-08-16 2009-01-15 Ghm Engineering EXHAUST BOLDER FOR AN INTERNAL COMBUSTION ENGINE
FR2925572B1 (en) * 2007-12-24 2010-02-12 Snecma Services METHOD FOR CHOOSING A SECTOR ARRANGEMENT FOR A TURBOMACHINE DISPENSER
US8070425B2 (en) * 2008-03-28 2011-12-06 Honeywell International Inc. Turbocharger with sliding piston, and having vanes and leakage dams
DE102008039085A1 (en) * 2008-08-21 2010-02-25 Daimler Ag Internal combustion engine with an exhaust gas turbocharger
DE102009004890A1 (en) * 2009-01-16 2010-07-22 Bosch Mahle Turbo Systems Gmbh & Co. Kg Charging device, particularly exhaust gas turbocharger for motor vehicle, has adjusting element, which is adjusted parallel to turbine wheel axis that is operatively connected with rotatably supported guide vane
US8113770B2 (en) * 2009-02-03 2012-02-14 Honeywell International Inc. Turbine assembly for an exhaust gas-driven turbocharger having a variable nozzle
DE102009018583A1 (en) * 2009-04-23 2010-10-28 Daimler Ag Internal combustion engine and method for operating an internal combustion engine
CN102770624B (en) * 2009-10-06 2015-02-25 康明斯有限公司 Variable geometry turbo machine
GB2474342A (en) * 2009-10-06 2011-04-13 Cummins Ltd Turbine nozzle component connection
FR2968717B1 (en) * 2010-12-14 2014-06-13 Faurecia Sys Echappement TURBINE HOUSING FOR TURBOCOMPRESSOR, TURBINE AND CORRESPONDING TURBOCOMPRESSOR.
CN102297016B (en) * 2011-08-15 2012-12-12 无锡凯迪增压器配件有限公司 Turbocharger for double-vane nozzle systems
DE102011121330A1 (en) * 2011-12-16 2013-06-20 Ihi Charging Systems International Gmbh Turbine for an exhaust gas turbocharger
WO2014175765A1 (en) * 2013-04-25 2014-10-30 Siemens Aktiengesellschaft Set of channel nozzles for a centripetal turboexpander
US9593690B2 (en) 2013-06-26 2017-03-14 Honeywell International Inc. Turbocharger with an annular rotary bypass valve
DE112014003991B4 (en) 2013-10-10 2023-06-29 Ihi Charging Systems International Gmbh Heat shield for an exhaust gas turbocharger and exhaust gas turbocharger and a method for producing a heat shield
SE539442C2 (en) * 2014-09-12 2017-09-26 Scania Cv Ab Turbine arrangement comprising two inlet pipes, each with bypass pipes, whose flow areas are variable by means of a common valve body
US9932886B2 (en) * 2016-02-17 2018-04-03 Honeywell International Inc. Turbocharger with rotary bypass valve operable to selectively configure the turbine volute as single-scroll or twin-scroll
CN110050115B (en) * 2017-02-28 2021-05-14 三菱重工发动机和增压器株式会社 Exhaust gas turbocharger
GB201909819D0 (en) * 2019-07-09 2019-08-21 Cummins Ltd Turbine assembly
JP7298525B2 (en) * 2020-03-24 2023-06-27 株式会社豊田自動織機 turbocharger
IL287648B2 (en) * 2021-10-28 2023-06-01 Gregory KATS Rotary engine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2861774A (en) * 1950-02-16 1958-11-25 Alfred J Buchi Inlet control for radial flow turbines
CH668455A5 (en) * 1984-06-29 1988-12-30 Bbc Brown Boveri & Cie Exhaust turbocharger with adjustable inlet - has blade ring on sleeve sliding on cylindrical surface
EP0571205B1 (en) * 1992-05-21 1997-03-05 Alliedsignal Limited Variable exhaust driven turbochargers
US5231831A (en) * 1992-07-28 1993-08-03 Leavesley Malcolm G Turbocharger apparatus
DE4242494C1 (en) * 1992-12-16 1993-09-09 Mercedes-Benz Aktiengesellschaft, 70327 Stuttgart, De Adjustable flow-guide for engine exhaust turbocharger - has axially-adjustable annular insert in sectors forming different kinds of guide grilles supplied simultaneously by spiral passages
US6521408B1 (en) * 1997-09-25 2003-02-18 National Institute Of Agrobiological Sciences Method for assessing a function of a gene
AU694393B2 (en) * 1996-09-26 1998-07-16 National Institute Of Agrobiological Resources, Ministry Of Agriculture, Forestry And Fisheries New high capacity binary shuttle vector
DE10212675B4 (en) * 2002-03-22 2006-05-18 Daimlerchrysler Ag Exhaust gas turbocharger in an internal combustion engine

Also Published As

Publication number Publication date
EP1725742A1 (en) 2006-11-29
WO2005040560A1 (en) 2005-05-06
US20080038110A1 (en) 2008-02-14

Similar Documents

Publication Publication Date Title
AU2003278524A1 (en) Sector-divided turbine assembly with axial piston variable-geometry mechanism
AU2003276753A1 (en) Wind turbine
EP1925795B8 (en) Split-cycle four stroke engine
AU2003235999A1 (en) Engine
AU2003294548A1 (en) External combustion rotary piston engine
AU2006292850A8 (en) An engine arrangement
AU2003262186A1 (en) Bearing assembly with an oil damper
AU2003252290A1 (en) Turbocharger
AU2003298668A1 (en) Epistemic engine
AU2003275557A1 (en) Engine
AU2003276751A1 (en) Windmill
AU2003293712A1 (en) Wind turbine
AU2002246270A1 (en) Oscillating-rotor engine
AU2003212219A1 (en) Engine
AU2002303047A1 (en) Axially aligned opposed piston engine
AU2003900549A0 (en) An assembly
AU2003239282A1 (en) Piston engine
AU2003273004A1 (en) Lightweight engine
AU2003207994A1 (en) Engine
AU2005903587A0 (en) Piston rotor engine
AU2003296047A1 (en) Hydraulic engine
AU2003297530A1 (en) Unitary rod/piston assembly
AUPS249302A0 (en) Turbine engine
WO2006090191A8 (en) Engines with amplifiers
AU2003906200A0 (en) Engine mechanism

Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase